Radne Raket 120
The Radne Raket 120 (English: Rocket) is a lightweight single cylinder, two-stroke aircraft engine used for powered hang gliders, paramotors and ultralight aircraft that is built by Radne Motor AB of Haninge, Sweden.[1][2][3]
Design and development
The Raket 120 features electronic ignition and a Walbro carburetor. It weighs 6.8 kg (15 lb) and, due to its 13,000 rpm redline usually drives a propeller through a 3.6:1 reduction drive. The engine is equipped with a centrifugal clutch to allow running the engine without turning the propeller.[1][2]
Variants
- Raket 120 Aero
- Model with recoil starter.[2]
- Raket 120 Aero ES
- Model with electric starter.[3]
Applications
Specifications (Raket 120 Aero)
Data from Radne and Wasp Systems[2][1]
General characteristics
- Type: two-stroke, single cylinder
- Bore: 60 mm (2.4 in)
- Stroke: 42 mm (1.7 in)
- Displacement: 118.8 cc (7.2 cu in)
- Dry weight: 6.8 kg (15 lb)
Components
Performance
- Power output: 14 hp (10 kW) at 9000 rpm
- Fuel consumption: 1.15 to 2 litres (0.25 to 0.44 imp gal; 0.30 to 0.53 USgal) per hour
References
External links
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